N219WN
Service difficulty reports · 301
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N219WN' AND registry_match = 'registration' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N219WN' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR SWAA2026101273388Battery Pack · no testBATTERY PACK M1674 FAILED A CAPACITY CHECK. R & R THE BATTERY PACK IAW AMM 33-51-06.SDR SWAA2026101245026Lanyard · misinstalledPASSENGER CABIN RIGHT OVERWING EMERGENCY HATCH ESCAPE LANYARD IMPROPERLY STOWED. STOWED RH OVER WING EXIT LIFE LINE REF AMM 25-61-10SDR SWAA2026101258144Lanyard · out of positionPASSENGER CABIN LEFT OVERWING EMERGENCY HATCH ESCAPE LANYARD IMPROPERLY STOWED. STOWED LH OVERWING EXIT LIFE LINE REF AMM 25-61-10SDR SWAA2026082408312Light · inoperativeLEFT OVERWING EMERGENCY EXIT EXTERIOR LIGHT INOPERATIVE. REMOVED AND REPLACED IAW AMM 33-51-04-960-801.SDR SWAA2026060909372Handle · looseL1 DOOR; LINER ASSIST HANDLE LOOSE. SECURED ASSIST HANDLE ON L1 DOOR. REF AMM 52-41-31.SDR SWAA2026060909369Handle · looseR1 DOOR; LINER ASSIST HANDLE LOOSE. SECURED R1 DOOR ASSIST HANDLE. REF AMM 52-41-31. CONFIRMED R1 DOOR ASSIST HANDLE SECURED IAW AMM 52-41-31.SDR SWAA2026012663947Skin · delaminatedRIGHT WING OUTBOARD AFT FLAP INBOARD AFT CORNER DELAMINATED. R & R RT WING OTBD TRAILING EDGE FLAP IAW AMM 27-51-21.SDR SWAA2025081403134Handle · crackedTHE RIGHT WING EMERGENCY EXIT DOOR HANDLE MOLDING IS CRACKED. REMOVED AND REPLACED THE RT WING EMERGENCY EXIT DOOR HANDLE MOLDING IAW AMM 52-22-51.SDR SWAA2025040119881Fitting · looseR1 FWD SERVICE DOOR; GIRT BAR FITTINGS; FWD AND AFT; LOOSE.<[01] TIGHTENED R1 FWD SERVICE DOOR GIRT BAR FITTINGS FWD AND AFT PER AMM 25-66-02-400-801; OPS CHECK CHECK GOOD.;[02] REJECT - BOTH FWD AND AFT GIRT BAR FITTINGS REMAIN LOOSE.;[03] TIGHTENED R1 FWD SESDR SWAA2025040119461Fuse · inoperativeFSD HEADER PANEL AND FWD LAV 'A' EMERGENCY EXIT LIGHT IN-OP<[01] REPLACED FUSE AT POWER SUPPLY OF BATTERY PACK M1675 AND PERFORMED GOOD EMERGENCY EXIT LIGHT TEST OF FWD HEADER PANEL AND FWD LAV 'A' IAW AMM 33-51-06-960-804.;[02] COMPLETESDR SWAA2025040202423Fitting · out of roundOUT OF ROUND HOLE FOUND ON BS727 INNER CHORD RH STR-18A UPPER FASTENER; MOST OUTBOARD LAYER OF STACK-UP. UNABLE TO COMPLETE NDI INSPECTION OF HOLE. <[01] REMOVED AND REPLACED UPPER FITTING BS 727 STR 18A IAW SRM 51-40-05; SRM 51-40-02; DWG #146A0062 REV-; DWG SDR SWAA2025040102305Floor Panel · delaminatedCABIN FLOOR PANEL 222BF HAS TOP SURFACE DELAMINATION.<[01] DUE TO THE EXTENT OF DAMAGE; REPLACED CABIN FLOOR PANEL 222BF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-00-50D ITEM96.;[02] VERIFIED JOB COMPLETESDR SWAA2025040102306Floor Panel · delaminatedCABIN FLOOR PANEL 221EF HAS TOP SURFACE DELAMINATION.<[01] DUE TO EXTENT OF DAMAGE; FLOOR PANEL 221EF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).;[02] VERIFIED CORRECTIVE ACTION ITEM 1.SDR SWAA2025040102307Floor Panel · delaminatedCABIN FLOOR PANEL 221GF HAS TOP SURFACE DELAMINATION.<[01] DUE TO THE EXTENT OF DAMAGE; REPLACED CABIN FLOOR PANEL 221GF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-00-50D ITEM 295.;[02] VERIFIED JOB COMPLETESDR SWAA2025040102308Floor Panel · delaminatedCABIN FLOOR PANEL 222CF HAS TOP SURFACE DELAMINATION.<[01] DUE TO EXTENT OF DAMAGE; FLOOR PANEL 222CF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).;[02] VERIFIED CORRECTIVE ACTION ITEM 1.SDR SWAA2025040201734Panel · debondedPANEL 621ZB FWD. CORNER DISBONDED.<[01] PANEL 621ZB WITH FWD CORNER DISBONDED WAS REPAIRED IAW SRM 57-41-01-2R-6.;[02] VERIFIED CORRECTIVE ACTION 1.SDR SWAA2025040200520Former · crackedWING TO BODY FAIRING FORMER IS CRACKED BS 500D BETWEEN STRINGER 19 AND 20 R/H<[01] REMOVED AND INSTALLED NEW FAIRING FORMER BS 500D BETWEEN STRINGER 19 AND 20 R/H IAW SRM 51-40-02-0G-0 AND DWG 116A3010 REV: A; 149A7101 REV: -.SDR SWAA2025040200176Panel · crackedSTA 540 BREAK PANEL IS CRACKED AT LBL 1; WL 208. <[01] REMOVED AND REPLACED WITH NEW BREAK PANEL AT 540 LBL 1; WL 208. REMOVE AND REINSTALL FLOOR PANEL 231UF TO ACCESS BREAK PANEL AT STA 540 LBL 1 WL 208. FLOOR PANEL 231UF WILL BE INSTALLED ON CARD#TTG8Q00Z5ESDR SWAA2025040200180Stiffener · crackedLH STAB RIB #4 STA 120.30 STIFFENER #2 AND #4 SHOWN CRACK<[01] REPAIRED LH STAB RIB #4 STA 120.30 STIFFENER #2 AND #4 IAW SRM 55-10-09-2R-4 REPAIR 4 AND SRM 55-10-09-2R-5 REPAIR 5 RESPECTIVELY.;[02] VERIFIED CORRECTIVE ACTION;[03] ALL RII STEPS COMPLETE.SDR SWAA2025040200511Rib · crackedRT HORIZ STAB L/E (341B) RIB AT LE STA 95.96 IS CRACKED AT UPPER AFT EDGE<[01] REMOVED AND REPLACED RIB AT R/H LE STAB STA 95.96 IAW SRM 51-40-02-0G-0 AND DWG. 186A1001-16; REV. A.;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.SDR SWAA2025040200510Rib · crackedLT HORIZ STAB L/E (331B) RIB AT LE STA 95.96 IS CRACKED AT LOWER AFT EDGE<[01] REPLACED A NEW RIB L/H HORIZONTAL STAB L/E (331B) AT L/E STA 95.96 IAW SRM 51-40-02 AND BOEING DWG 186A1001 SH 10SDR SWAA2025040100393Skin · crackedCRACK ON RH LOWER HORIZONTAL STABILIZER SKIN. AT STAB STA 193.90; 11.75' FROM FWD EDGE; .25' IN LENGTH (MARKED)<[01] 'REPAIRED PER EA 25-155-00704 WITH REPETITIVE INSPECTION PROGRAM DEFINED IN EA 25-155-00704-INSP.';[02] COMPLETESDR SWAA2025040100172Floor Panel · pulledFLOOR PANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO THE EXTENT OF DAMAGE; FABRICATED NEW FLOOR PANEL 241DF USING BMS 4-17 TY6 LOT#1594495-1; INSTALLED INSERTS USING BMS 5-107 LOT#AK4FA2417A/A; CURED WITH THERMOMETER ID:ATS2208 CAL DUE 10/2025SDR SWAA2025040100173Floor Panel · pulledFLOOR PANEL 241EF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO THE EXTENT OF DAMAGE; FABRICATED NEW FLOOR PANEL 241EF USING BMS 4-17 TY6 LOT#1594495-1; INSTALLED INSERTS USING BMS 5-107 LOT#AK4FA2417A/A; CURED WITH THERMOMETER ID:ATS2208 CAL DUE 10/2025SDR SWAA2025040100178Floor Panel · pulledFLOOR PANEL 242DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATION OF NEW 242DF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED PER [SRM 53-00-50-2R-0-A00938 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)]<BR><BR>ATTACHED CURE SHEET TO THIS FAULT.SDR SWAA2025040299338Vapor Barrier · crackedLEFT HAND BS 663 COMPOSITE VAPOR BARRIER HAS MULTIPLE CRACKS AT LBL 28; WL 164. <[01] L/H VAPOR BARRIER BS663 MULTIPLE CRACKS AT LBL 28 WL 164 WERE REPAIRED IAW SRM 51-70-04-2R-10.SDR SWAA2024111859797Battery Pack · inoperativeL1; R1; AND FWD GALLEY EMERGENCY EXIT LIGHTS INOP.<[01] REMOVED AND REPLACED LH FWD BATTERY PACK IAW AMM 33-51-06. OP CHECK GOOD.SDR SWAA2024101748013Lamp · inoperativeRH AFT SLIDE EMERGENCY LIGHT INOP<[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-04-960-801-NG (RH AFT SLIDE LIGHT - LAMP REPLACEMENT - PERMANENT)]SDR SWAA2024070810054Tailpipe · fire#2 ENGINE TAIL PIPE FIRE AT GATE<[01] LP 2602505 AP 3395119 INSPECTED INLET AND EXHAUST FOUND OIL ACCUMULATION IN THE CENTER EXHAUST PLUG CAVITY NO OTHER DEFECTS NOTED. OIL CONSUMPTION AND PRESSURE ARE WITHIN NORMAL LIMITS. REF FIM 71-05 TASK 811. POWERPLANT ESDR SWAA2024052889533Idg · faultedDURING CRUISE FLIGHT @FL370 #2 IDG SHOWED SOURCE OFF LIGHT AND TRANSFER BUS OFF LIGHT ILLUMINATED.<[01] R & R #2 ENG IDG IAW AMM 24-11-11. NO DEFECTS NOTED.SDR SWAA2024022154126Sign · wrong partLOWER RT OVER WING EMERGENCY EXIT SIGN DOESN'T HAVE A DIRECTION ARROW.<[01] REMOVED AND REPLACED SIGN IAW AMM 33-51-01SDR SWAA2024022154125Lens · missingEMERGENCY EXIT LIGHT LENS IS MISSING AT 4ABC.<[01] INSTALLED NEW COVER IAW AMM 25-24-31SDR SWAA2024020247613Slide · out of adjustAFT SERVICE DOOR SLIDE LOOSE<[01] REMOVED SLIDE WITH COMPARTMENT FROM DOOR AND ADJUSTED. SLIDE SECURE AND GAUGE VISIBLE. REINSTALLED SLIDE IAW MT#725-61-06.SDR SWAA2023112723382Lens · looseCABIN AISLE LIGHT ROW 11 DEF COVER CAME OFF<[01] OK TO CONTINUE PER MEL 33-15-02 SP1;[02] INSTALLED LENS IAW AMM 33-51-03SDR SWAA2023102714069Seal · crackedRIGHT HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL CRACKED.<[01] REMOVED AND REPLACED RIGHT HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL PER AMM 53-31-31.SDR SWAA2023100908937Fastener · brokenFORWARD SERVICE DOOR FIRST BAR HOLDER BROKEN<[01] REMOVED AND REPLACED FASTENERS ON FWD SERVICE DOOR SLIDE GIRT BAR AFT HOOK PER SRM 51-40-02SDR SWAA2023083195728Light · out of adjustFWD SERVICE DOOR EMERGENCY LIGHT EXIT LIGHT COVER FALLS OFF.<[01] R&R FWD SERVICE DOOR EMERGENCY EXIT LIGHT ASSEMBLY REF AMM 33-1-01.SDR SWAA2023071777818Strap · looseRH EMERGENCY EXIT ASSIST STRAP COMPARTMENT NOT SECURE<[01] RE-SECURED RH EMERGENCY EXIT ASSIST STRAP COMPARTMENT; PER AMM 52-22-51SDR SWAA2023031309391Track · corrodedCORROSION TRACK RBBL 13.84 LOCATED BTW STA 787 TO STA 807 PLUS 3 INCHES WL 157.5 AT AFT CARGO COMPARTMENT 2023-<[01] FAULT RESOLVED ON OTHER FAULT SEE TTG8Q00HU0PW;[02] FAULT RESOLVED ON OTHER FAULT SEE TTG8Q00HU0PWSDR SWAA2023031304028Bracket · brokenBROKEN SUPPORT BRACKET ON ACCESS PANEL 551FB LT WING 2023-113098<[01] REPLACED SUPPORT BRACKET ON ACCESS PANEL 551FB LT WING IAW B737-700 SRM 51-40-02 AND DRAWING # 115A2710 REV: B. TOOK MEASURE OF CRACK IS : L= 0.950?. TOOL USED CALIPER P/N: 500-752-20; S/N:BSDR SWAA2023031303095Support · corrodedCORROSION SUPPORT ZEE LOCATED BTW 737D TO STA 767 AT LEVEL STR 25R WL 156.5 AT AFT CARGO COMPARTMENT 2023-113083<[01] REPLACED SUPPORT ZEE LOCATED BTW 727 TO STA 767 AT LEVEL STR 25R WL 156.5 AT AFT CARGO COMPARTMENT AND FASTENERS I.A.W B737-700 SRM 51-40-02 ASDR SWAA2023031303101Angle · crackedCUSTOMER REQUEST AAI CRACK ON ANGLE LOCATED RACEWAY PANEL AREA CAPTAIN SIDE AT COCKPIT 2023-113089<[01] TOOL USED: TEMPERATURE CONTROLLER: P/N: 48VFL11; S/N: AE-31448; DUE DATE: 14-JUN-23.;[02] REPLACED ANGLE LOC. RACEWAY PANEL AREA CAPTAIN SIDE AT COCKPIT IAWSDR SWAA2023031303092Angle · crackedCRACK ANGLE LOCATED BTW STA 907 TO STA 927 STR 25R TO STR 27R FWD POSITION AFT CARGO COMPARTMENT 2023-113080<[01] REPLACED ANGLE LOCATED BTW STA 907 TO STA 927 STR 25R TO STR 27R FWD POSITION AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9SDR SWAA2023031003096Track · corrodedCORROSION TRACK RBBL 13.84 LOCATED BTW STA 787 TO STA 807 PLU 3 INCHES WL 157.5 AT AFT CARGO COMPARTMENT 2023-113084<[01] PERFORMED REPAIR ON CARGO TRACK SECTION RBBL 13.84 LOCATED BTW BS747 MORE 7? TO BS887 I.A.W B737-700 SRM 53-00-53-2R-3 REPAIR 3 FIGURE 203SDR SWAA2023031302656Plate · crackedCRACK REAR SPAR CORRUGATED PLATE LOCATED AT IRSS 216 AT LT WING 2023-113071<[01] REPLACED REAR SPAR CORRUGATE PLATE LOCATED AT IRSS 216 AT LT WING I.A.W. B737-700 SRM 51-10-02 AND SRM 51-40-02 AND DWG 115A2001 SHEET 30 REV.A. DUE TO NOT FOUND ALLOWABLE DAMAGE SDR SWAA2023031302332Track · crackedCRACK CARGO TRACK LOCATED BS747 RBL13 AND WL156 AT AFT CARGO COMPARTMENT 2023-113064<[01] TOOL USED DIGITAL CALIPER P/N: 500-197-30 S/N: B20189511 DUE DATE: 12-OCT-23.;[02] PERFORMED REPAIR ON CARGO TRACK LOCATED BTW BS727E MORE 7.5? TO BS747 MORE 11? RBL13 ANSDR SWAA2023031302655Angle · crackedCRACK ANGLE LOCATED BTW STA 907 TO STA 927 STS 25L TO STR 27L AFT CARGO COMPARTMENT 2023-113072<[01] REPLACED ANGLE LOCATED BTW STA 907 TO STA 927 STS 25L TO STR 27L AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-20-02 ITEM 9 AND DWG 147A7221 REV. -. SDR SWAA2023031302657Support · crackedCRACK ANGLE - SUPPORT LOCATED STA 867 AT LEVEL STR 26L AFT CARGO COMPARTMENT 2023-113074<[01] REPLACED ANGLE - SUPPORT LOCATED STA 867 AT LEVEL STR 26L AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02 ITEM 9 AND DWG #149A8102 REV:-;[02] REPLACED ANGLE - SUPPOSDR SWAA2023031302329Panel · delaminatedDELAMINATED ACCESS PANEL 193AR AT LOWER FUSELAGE 2023-113052<[01] TOOL USED: CALIPER PN: 500-197-30 B20189526 DUE DATE: 20/DEC/23.;[02] TOOL USED HOT BONDER P/N: HCS9200B P/N: 18165044; DUE DATE: 28-FEB-23;[03] TOOL USED: SCALE PN: SPX621; SN: 8340225441; DUE SDR SWAA2023031302331Track · crackedCRACK CARGO TRACK LOCATED BS767 LBL17 AND WL156 AT AFT CARGO COMPARTMENT 2023-113063<[01] TOOL USED: DIGITAL CALIPER; P/N: 500-193-30; S/N:0000293; DUE DATE:12-OCT-23.;[02] PERFORMED PERMANENT REPAIR CARGO TRACK LOCATED BS747 TO BS 787 LBL17 AND WL156 AT AFT C
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